Controlled Aerodynamic Loads on a Slender Axisymmetric Body at High Incidence

[1]  Laser Doppler Velocimeter measurements of leeward flowfields on slender bodies at large angle-of-attack , 1977 .

[2]  Russ Stucke High angle-of-attack yaw control using strakes on blunt-nose bodies , 2006 .

[3]  R. C. Nelson,et al.  High Angle-of-Attack Aerodynamics on a Slender Body with a Jet Plume , 1975 .

[4]  D. Degani,et al.  Asymmetric Vortices on a Slender Body of Revolution , 1991 .

[5]  C. Schnepf,et al.  Numerical study on the impact of a maneuver on the Phantom-Yaw-Effect in transonic flow , 2018, 2018 Applied Aerodynamics Conference.

[6]  A. Wardlaw,et al.  The secondary separation region on a body at high angles of attack , 1982 .

[7]  Rajan Kumar,et al.  Effect of Controlled Imperfections on the Vortex Asymmetry of a Conical Body , 2018, AIAA Journal.

[8]  D. Williams,et al.  Control of asymmetric vortices around a cone-cylinder geometry with unsteady base bleed , 1989 .

[9]  D. G. Murri,et al.  Forebody vortex management for yaw control at high angles of attack , 1987 .

[10]  I. Wygnanski,et al.  Re-orienting the Turbulent flow over an Inclined Cylinder of Finite Aspect ratio , 2018, 2018 Flow Control Conference.

[11]  Tom McLaughlin,et al.  Experimental Study of Open Loop Plasma Actuation on a von Karman Ogive , 2012 .

[12]  Thomas J. Lambert,et al.  Aerodynamic Flow Control of Axisymmetric Bluff Body by Coupled Wake Interactions , 2018, AIAA Journal.

[13]  Ari Glezer,et al.  A Six Degrees of Freedom Dynamic Wire-Driven Traverse , 2016 .